View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68095U 26145.48379171 +.00000000 +00000-0 +65300-3 0 00006
2 68095 53.1594 181.2400 0001370 68.4890 291.6259 15.34402424 02
| Epoch (UTC): | 25 May 2026 11:36:39 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.2400° |
| argument of perigee: | 68.4890° |
| revolutions per day: | 15.34402424 |
| mean anomaly at epoch: | 291.6259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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